导弹姿态控制系统动态测试研究

Study on Dynamic Measurement of Missile Attitude Control System

分析了某型导弹姿态控制系统频域动态测试遇到的问题及时域测试结果 ,建立了姿态控制系统测试模型 ,并研究了其在时域内的快速动态测试方法。实验表明 ,所建立的测试系统模型是合理的 。

The problems of a missile attitude control system encountered in frequency domain dynamic measurement and the time domain measurement results are analyzed. The testing model of attitude control system is established, and the fast dynamic testing method in time domain is studied. The experimental results show that the testing model is reasonable, and can reflect the modes of attitude control system correctly.